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SAE AIR4065 Rev A

Propeller/Propfan In-Flight Thrust Determination
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SAE AIR4065 Rev A

Propeller/Propfan In-Flight Thrust Determination

PUBLISH DATE 2012
PAGES 216
SAE AIR4065 Rev A
AIR 4065, "Propeller/Propfan In-Flight Thrust Determination" addresses steady state propeller thrust as applied to aircraft which are usually powered by gas turbine engines. It includes theory, examples and methods which have been used. Specifically two methods are discussed, the "J" or traditional J,C p ,C t , η method including the SBAC variation and a new method we call the "Theta" method which is dependent on knowing blade angle, power/torque and flight Mach number. Implementation guidelines are offered as well as overall approaches to flight testing. Appendices include expansions on theory and testing as well as examples.
SDO SAE: SAE International
Document Number AIR4065
Publication Date May 29, 2012
Language en - English
Page Count 216
Revision Level A
Supercedes
Committee
Publish Date Document Id Type View
May 29, 2012 AIR4065A Revision
June 1, 1993 AIR4065 Revision